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IRIDIUM 57

NORAD 25273 Payload LEO 1998-019B ● Active
CONNECTING… LEO · NORAD 25273
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Altitude (km)
Speed (km/s)
Latitude
Longitude
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🛰️ Orbital Parameters
Perigee
770 km
Apogee
773 km
Inclination
86.4°
Period
100.3 min
Mean Motion
14.36183736 rev/day
TLE Epoch
2026-06-19 22:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude772 km
Orbital Velocity26,893 km/h
Velocity7.47 km/s
Orbital Period100 minutes
Orbits / Day14.36
Eccentricity0.0002
Semi-Major Axis7,143 km
Est. Orbital Lifetime~25–100 years
🚀 Launch & Identity
Country / Operator
🇺🇸 Iridium Communications (United States)
Launch Date
1998-03-30
Launch Site
Vandenberg SFB, California
Int'l Designator
1998-019B
Object Type
Payload
RCS Size
Large (>1 m²)
🔗 Constellation / Groups
iridium
📖 About This Object
IRIDIUM 57 is an active satellite operated by Iridium Communications (United States), launched on 1998-03-30 from Vandenberg SFB, California. With over 28 years in orbit, it has far exceeded many satellites’ design lifetimes. It orbits in Low Earth Orbit (LEO) at altitudes between 770 km and 773 km with an inclination of 86.4°. It travels at approximately 26,893 km/h (7.47 km/s), completing one full orbit every 100 minutes — that’s roughly 14.36 orbits per day. Its near-circular orbit (eccentricity close to zero) means it maintains a very consistent altitude throughout each revolution. It is part of the Iridium constellation group. At its current altitude, the estimated orbital lifetime before atmospheric re-entry is ~25–100 years. Orbital Radar tracks IRIDIUM 57 in real time using the latest two-line element set (TLE) data, providing live position, altitude, speed and orbital path updated continuously.
🌍 Orbit Context
IRIDIUM 57 orbits at an average altitude of 772 km in the mid-LEO band, where atmospheric drag is minimal but radiation exposure remains manageable. Objects at this altitude persist for decades to centuries, making debris mitigation critical. This regime is popular for remote sensing constellations and scientific instruments that need stable, long-duration orbits. Within ±50 km of IRIDIUM 57’s average altitude, there are currently 397 active payloads and 2,109 tracked debris or rocket body fragments — notable neighbours include ONEWEB-0179, ONEWEB-0455. With an inclination of 86.4°, IRIDIUM 57 passes over latitudes between 86.4°N and 86.4°S, providing near-global coverage including the polar regions. Polar and near-polar orbits are used for reconnaissance, weather monitoring and Earth-observation missions that need to image every part of the planet. United States operates approximately 12,360 active satellites in total, of which 148 share a similar altitude band with IRIDIUM 57.
🔗 Iridium NEXT Constellation

This satellite is part of the Iridium NEXT constellation, a fleet of 66 operational cross-linked LEO satellites (plus spares) providing global voice, data and IoT connectivity. Iridium operates at approximately 780 km altitude across six polar orbital planes, ensuring coverage over the entire Earth surface including oceans and polar regions. The second-generation NEXT satellites replaced the original constellation between 2017–2019 and support Iridium Certus broadband and the Aireon ADS-B aircraft tracking payload.

❓ Frequently Asked Questions
IRIDIUM 57 orbits in Low Earth Orbit (LEO) at altitudes between 770 km (perigee) and 773 km (apogee), with an average altitude of approximately 772 km. It completes one orbit every 100 minutes, travelling at approximately 26,893 km/h (16,711 mph).
IRIDIUM 57 is operated by Iridium Communications (United States). It is catalogued by the U.S. Space Surveillance Network under NORAD ID 25273. You can track IRIDIUM 57 in real time on Orbital Radar’s live tracker or browse all operators in the operator directory.
IRIDIUM 57 was launched on 1998-03-30 from Vandenberg SFB, California, primarily used for polar and sun-synchronous orbit launches due to its southward ocean trajectory from California. At its current altitude, the estimated remaining orbital lifetime is: ~25–100 years. View the full satellite launch log.
Yes — Orbital Radar tracks IRIDIUM 57 (NORAD ID 25273) using the latest TLE (two-line element set) data from Space-Track and CelesTrak. Open the live tracker to see its current position, altitude, speed and orbital path updated in real time. You can also browse the satellite directory to find other tracked objects.
IRIDIUM 57 travels at approximately 26,893 km/h (16,711 mph) — roughly 7.47 km/s. It completes 14.36 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 29 sunrises and sunsets every 24 hours.
IRIDIUM 57 is a member of the Iridium constellation. Satellites in this group work together to provide coordinated coverage, typically in similar orbital planes at comparable altitudes. You can view all Iridium satellites on Orbital Radar’s live tracker.